Abstract An integral method is proposed for calculating a jet propagating from the turbofan engine thrust reverser and interacting with a stream formed as a result of the after-landing aircraft run. The calculation results for the PS-90 engine are presented. The calculation data obtained show that the mathematical model developed adequately describes a qualitative pattern of main parameter variation in the sector jet propagating in a stream.
Integral method for calculating a turbofan engine thrust reverser jet interacting with an external stream
Russian Aeronautics (Iz VUZ) ; 53 , 2 ; 212-220
2010-06-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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